View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 57125U 26145.57630453 +.00000000 +00000-0 +86355-5 0 00006
2 57125 43.0031 189.0019 0001654 285.6947 74.3723 15.27571425 03
| Epoch (UTC): | 25 May 2026 13:49:52 |
| Eccentricity: | 0.0001654 |
| inclination: | 43.0031° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 189.0019° |
| argument of perigee: | 285.6947° |
| revolutions per day: | 15.27571425 |
| mean anomaly at epoch: | 74.3723° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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